FR3015574B1 - Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif - Google Patents
Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif Download PDFInfo
- Publication number
- FR3015574B1 FR3015574B1 FR1363316A FR1363316A FR3015574B1 FR 3015574 B1 FR3015574 B1 FR 3015574B1 FR 1363316 A FR1363316 A FR 1363316A FR 1363316 A FR1363316 A FR 1363316A FR 3015574 B1 FR3015574 B1 FR 3015574B1
- Authority
- FR
- France
- Prior art keywords
- helicopter
- corresponding control
- control device
- automatically controlling
- turbomotor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/20—Adaptations of gas-turbine plants for driving vehicles
- F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
- B64D31/02—Initiating means
- B64D31/06—Initiating means actuated automatically
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/02—Shutting-down responsive to overspeed
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/02—Plural gas-turbine plants having a common power output
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/329—Application in turbines in gas turbines in helicopters
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/02—Purpose of the control system to control rotational speed (n)
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/07—Purpose of the control system to improve fuel economy
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/09—Purpose of the control system to cope with emergencies
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/09—Purpose of the control system to cope with emergencies
- F05D2270/093—Purpose of the control system to cope with emergencies of one engine in a multi-engine system
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/13—Purpose of the control system to control two or more engines simultaneously
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Turbines (AREA)
- Control Of Velocity Or Acceleration (AREA)
Abstract
L'invention concerne un procédé de commande automatique d'un régime de fonctionnement d'un turbomoteur d'un hélicoptère, comprenant une étape (10) de réception de données (27, 28, 29) représentatives du vol de l'hélicoptère ; une étape (11) de sélection du turbomoteur pour lequel un changement de régime serait le plus pertinent ; une étape (12) de détermination d'un régime de fonctionnement dudit turbomoteur, dit régime élu, choisi parmi une pluralité de régimes de fonctionnement prédéterminés ; et une étape (14) de commande du régime de fonctionnement dudit turbomoteur audit régime élu. L'invention concerne également un dispositif de commande correspondant.
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1363316A FR3015574B1 (fr) | 2013-12-20 | 2013-12-20 | Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif |
CA2933357A CA2933357C (fr) | 2013-12-20 | 2014-12-15 | Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif |
US15/104,470 US10435167B2 (en) | 2013-12-20 | 2014-12-15 | Method for automatically controlling the operating speed of a helicopter turboshaft engine, corresponding control device and helicopter provided with such a device |
PCT/FR2014/053351 WO2015092252A1 (fr) | 2013-12-20 | 2014-12-15 | Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif |
EP14827845.0A EP3084175B1 (fr) | 2013-12-20 | 2014-12-15 | Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif |
PL14827845T PL3084175T3 (pl) | 2013-12-20 | 2014-12-15 | Sposób automatycznego sterowania trybem pracy silnika turbinowego śmigłowca, odpowiednie urządzenie sterujące i śmigłowiec wyposażony w takie urządzenie |
RU2016125745A RU2693957C1 (ru) | 2013-12-20 | 2014-12-15 | Способ автоматического управления рабочим режимом газотурбинного двигателя вертолета, соответствующее устройство управления и вертолет, оснащенный таким устройством |
KR1020167017263A KR102263904B1 (ko) | 2013-12-20 | 2014-12-15 | 헬리콥터 터보샤프트 엔진의 작동 속도를 자동 제어하는 방법, 대응하는 제어 장치 및 그 장치를 구비한 헬리콥터 |
CN201480068802.4A CN105829680B (zh) | 2013-12-20 | 2014-12-15 | 自动控制直升机涡轮轴发动机的运行速度的方法,对应的控制设备以及具有该设备的直升机 |
JP2016540596A JP6608825B2 (ja) | 2013-12-20 | 2014-12-15 | ヘリコプタのターボシャフトエンジン、対応する制御デバイス、およびそのようなデバイスが設けられたヘリコプタの作動速度を自動的に制御するための方法。 |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1363316A FR3015574B1 (fr) | 2013-12-20 | 2013-12-20 | Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif |
FR1363316 | 2013-12-20 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3015574A1 FR3015574A1 (fr) | 2015-06-26 |
FR3015574B1 true FR3015574B1 (fr) | 2019-05-03 |
Family
ID=50290026
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1363316A Active FR3015574B1 (fr) | 2013-12-20 | 2013-12-20 | Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif |
Country Status (10)
Country | Link |
---|---|
US (1) | US10435167B2 (fr) |
EP (1) | EP3084175B1 (fr) |
JP (1) | JP6608825B2 (fr) |
KR (1) | KR102263904B1 (fr) |
CN (1) | CN105829680B (fr) |
CA (1) | CA2933357C (fr) |
FR (1) | FR3015574B1 (fr) |
PL (1) | PL3084175T3 (fr) |
RU (1) | RU2693957C1 (fr) |
WO (1) | WO2015092252A1 (fr) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3026435B1 (fr) * | 2014-09-29 | 2016-10-21 | Turbomeca | Dispositif et procede de test d'integrite d'un systeme de reactivation rapide d'un turbomoteur d'un helicoptere |
US10604268B2 (en) * | 2017-02-22 | 2020-03-31 | Pratt & Whitney Canada Corp. | Autothrottle control for turboprop engines |
FR3082225B1 (fr) * | 2018-06-07 | 2020-06-05 | Safran Helicopter Engines | Systeme propulsif asymetrique a recuperation de chaleur |
CN109228805B (zh) * | 2018-08-22 | 2021-07-09 | 上海工程技术大学 | 一种汽车轮胎紧急自动充气装置 |
CN109236475B (zh) * | 2018-11-15 | 2020-07-17 | 中国直升机设计研究所 | 一种单发直升机涡轴发动机的电气控制系统 |
US11725597B2 (en) * | 2019-02-08 | 2023-08-15 | Pratt & Whitney Canada Corp. | System and method for exiting an asymmetric engine operating regime |
US11299286B2 (en) | 2019-05-15 | 2022-04-12 | Pratt & Whitney Canada Corp. | System and method for operating a multi-engine aircraft |
CN114508435A (zh) * | 2022-02-17 | 2022-05-17 | 上海东古智能科技有限公司 | 一种双冲程汽油航空发动机的控制系统 |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2188960C1 (ru) * | 2001-08-20 | 2002-09-10 | Кондрашов Борис Михайлович | Способ преобразования энергии в силовой установке (варианты), струйно-адаптивном двигателе и газогенераторе |
JP2005247008A (ja) * | 2004-03-01 | 2005-09-15 | Yamaha Motor Co Ltd | 無人ヘリコプタ用制御装置 |
FR2914697B1 (fr) * | 2007-04-06 | 2012-11-30 | Turbomeca | Dispositif d'assistance aux phases transitoires d'acceleration et de deceleration |
US8200375B2 (en) * | 2008-02-12 | 2012-06-12 | Stuckman Katherine C | Radio controlled aircraft, remote controller and methods for use therewith |
FR2950109B1 (fr) * | 2009-09-17 | 2012-07-27 | Turbomeca | Turbomoteur a arbres paralleles |
ITTO20090079U1 (it) | 2009-06-10 | 2010-12-11 | Agusta Spa | Sistema per la gestione ed il controllo della velocita' di uno o piu' rotori di un aeromobile atto a volare a punto fisso |
FR2950324B1 (fr) * | 2009-09-23 | 2011-08-26 | Eurocopter France | Procede et dispositif d'aide au pilotage d'un aeronef en cas de pannes d'un indicateur de premiere limitation |
US20110154805A1 (en) * | 2009-12-31 | 2011-06-30 | Craig Heathco | Power augmentation system for an engine powered air vehicle |
FR2967132B1 (fr) * | 2010-11-04 | 2012-11-09 | Turbomeca | Procede d'optimisation de la consommation specifique d'un helicoptere bimoteur et architecture bimoteur dissymetrique a systeme de regulation pour sa mise en oeuvre |
FR2983319B1 (fr) * | 2011-11-25 | 2014-02-07 | Turbomeca | Procede et systeme de regulation de puissance en cas de defaillance d'au moins un moteur d'aeronef |
US8768598B2 (en) * | 2011-12-26 | 2014-07-01 | Textron Innovations Inc. | Dual gain digital engine control |
FR2986573B1 (fr) * | 2012-02-07 | 2014-02-21 | Eurocopter France | Procede automatique de regulation d'un groupe de motorisation d'aeronef, dispositif et aeronef |
FR2986572B1 (fr) * | 2012-02-07 | 2016-04-29 | Eurocopter France | Procede automatique de regulation d'un groupe de motorisation d'aeronef, dispositif et aeronef |
US9091616B2 (en) * | 2013-06-06 | 2015-07-28 | Honeywell International Inc. | Engine operations support systems and methods for reducing fuel flow |
US10850863B2 (en) * | 2014-03-04 | 2020-12-01 | Pratt & Whitney Canada Corp. | System and method for operating a multi-engine aircraft in an auxiliary power unit mode |
US20150266589A1 (en) * | 2014-03-24 | 2015-09-24 | Honeywell International Inc. | Aircraft systems and methods with green fuel tanks |
US9547990B2 (en) * | 2014-08-21 | 2017-01-17 | Honeywell International Inc. | Rotary-wing aircraft emergency landing control |
-
2013
- 2013-12-20 FR FR1363316A patent/FR3015574B1/fr active Active
-
2014
- 2014-12-15 EP EP14827845.0A patent/EP3084175B1/fr active Active
- 2014-12-15 CA CA2933357A patent/CA2933357C/fr active Active
- 2014-12-15 US US15/104,470 patent/US10435167B2/en active Active
- 2014-12-15 KR KR1020167017263A patent/KR102263904B1/ko active IP Right Grant
- 2014-12-15 CN CN201480068802.4A patent/CN105829680B/zh active Active
- 2014-12-15 WO PCT/FR2014/053351 patent/WO2015092252A1/fr active Application Filing
- 2014-12-15 RU RU2016125745A patent/RU2693957C1/ru active
- 2014-12-15 PL PL14827845T patent/PL3084175T3/pl unknown
- 2014-12-15 JP JP2016540596A patent/JP6608825B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
WO2015092252A1 (fr) | 2015-06-25 |
RU2693957C1 (ru) | 2019-07-08 |
EP3084175A1 (fr) | 2016-10-26 |
US20160311548A1 (en) | 2016-10-27 |
CN105829680A (zh) | 2016-08-03 |
EP3084175B1 (fr) | 2020-06-17 |
US10435167B2 (en) | 2019-10-08 |
KR20160098289A (ko) | 2016-08-18 |
CN105829680B (zh) | 2018-12-14 |
KR102263904B1 (ko) | 2021-06-11 |
FR3015574A1 (fr) | 2015-06-26 |
RU2016125745A (ru) | 2018-01-25 |
CA2933357A1 (fr) | 2015-06-25 |
JP6608825B2 (ja) | 2019-11-20 |
CA2933357C (fr) | 2022-03-29 |
PL3084175T3 (pl) | 2020-11-02 |
JP2017502201A (ja) | 2017-01-19 |
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